Date: May 12th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2010/130/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4762138
62                 A    =         6725606
59  meter
 Y    =       -2480391
75  meter          E    =           
0007306
 Z    =        4054029
51                 I    =           51
94271
 XDOT =        130
489278                 Wp   =           11
39960
 YDOT =      -6634
425352  meter/sec      RA   =           63
74874  deg
 ZDOT =      -3897
693345                 TA   =          118
66997
                                          MA   =          118
59650
                                          Ha   =            190
059  n
mi
                                          Hp   =            186
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15623814
35                 X    =        -4753742
56
 Y    =       -8137768
21  feet           Y    =        -2533597
96  meter
 Z    =       13300621
77                 Z    =         4030915
00
 XDOT =        428
114430                 XDOT =         223
601522
 YDOT =     -21766
487375  feet/sec       YDOT =       -6632
445439  meter/sec
 ZDOT =     -12787
707826                 ZDOT =       -3896
833391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17412711
67                 X    =        -5307394
52
 Y    =       -3092780
01  feet           Y    =         -942679
35  meter
 Z    =       13208541
55                 Z    =         4025963
46
 XDOT =      -6226
316368                 XDOT =       -1897
781229
 YDOT =     -19659
642395  feet/sec       YDOT =       -5992
259002  meter/sec
 ZDOT =     -12784
349935                 ZDOT =       -3896
669860


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10130
45719941  
00016717  00000-0  10270-3 0  9002
2 25544  51
6425  64
2228 0010292 298
2222  61
7902 15
73835137 17534


Satellite: ISS
Catalog Number: 25544
Epoch time:      10130
45719941   =   yrday
fracday
Element set:     900
Inclination:       51
6425  deg
RA of node:        64
2228  deg
Eccentricity:     
0010292     
Arg of perigee:   298
2222  deg
Mean anomaly:      61
7902  deg
Mean motion:   15
73835137  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1753
Checksum:              290


Coasting Arc #2 (Orbit 1768)
---------------------------------------

Vector Time (GMT): 2010/131/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         428998
61                 A    =         6727534
63  meter
 Y    =        5796498
48  meter          E    =           
0006493
 Z    =        3379009
93                 I    =           51
93640
 XDOT =      -5678
206611                 Wp   =           35
20104
 YDOT =      -2300
540237  meter/sec      RA   =           58
68685  deg
 ZDOT =       4668
124332                 TA   =            4
46794
                                          MA   =            4
46215
                                          Ha   =            190
152  n
mi
                                          Hp   =            186
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1407475
75                 X    =          347734
29
 Y    =       19017383
47  feet           Y    =         5800841
30  meter
 Z    =       11085990
58                 Z    =         3380896
86
 XDOT =     -18629
286782                 XDOT =       -5674
736894
 YDOT =      -7547
704190  feet/sec       YDOT =       -2364
018096  meter/sec
 ZDOT =      15315
368542                 ZDOT =        4640
547393

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7248442
55                 X    =         2209325
29
 Y    =       17633326
59  feet           Y    =         5374637
95  meter
 Z    =       11093553
22                 Z    =         3381315
02
 XDOT =     -18856
657382                 XDOT =       -5747
509170
 YDOT =      -1813
254623  feet/sec       YDOT =        -552
680009  meter/sec
 ZDOT =      15205
523649                 ZDOT =        4634
643608


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10131
47313299  
00016717  00000-0  10270-3 0  9012
2 25544  51
6435  59
0072 0010262 301
2610  58
7547 15
73883303 17693


Satellite: ISS
Catalog Number: 25544
Epoch time:      10131
47313299   =   yrday
fracday
Element set:     901
Inclination:       51
6435  deg
RA of node:        59
0072  deg
Eccentricity:     
0010262     
Arg of perigee:   301
2610  deg
Mean anomaly:      58
7547  deg
Mean motion:   15
73883303  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1769
Checksum:              289


Coasting Arc #3 (Orbit 1783)
---------------------------------------

Vector Time (GMT): 2010/132/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5112384
37                 A    =         6725377
96  meter
 Y    =        1517116
82  meter          E    =           
0003866
 Z    =       -4094172
89                 I    =           51
91222
 XDOT =       1121
326758                 Wp   =          339
12780
 YDOT =       6580
110839  meter/sec      RA   =           53
52182  deg
 ZDOT =       3840
922151                 TA   =          330
18309
                                          MA   =          330
20511
                                          Ha   =            190
553  n
mi
                                          Hp   =            186
058

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16772914
60                 X    =         5114928
92
 Y    =        4977417
40  feet           Y    =         1574301
02  meter
 Z    =      -13432325
75                 Z    =        -4069330
10
 XDOT =       3678
893564                 XDOT =        1029
004511
 YDOT =      21588
290154  feet/sec       YDOT =        6592
133757  meter/sec
 ZDOT =      12601
450626                 ZDOT =        3846
145807

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17549798
20                 X    =         5349178
49
 Y    =        -870799
09  feet           Y    =         -265419
56  meter
 Z    =      -13333379
74                 Z    =        -4064014
14
 XDOT =      10472
065858                 XDOT =        3191
885673
 YDOT =      17905
258767  feet/sec       YDOT =        5457
522872  meter/sec
 ZDOT =      12622
294871                 ZDOT =        3847
275477


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10132
42555783  
00016717  00000-0  10270-3 0  9025
2 25544  51
6437  54
1175 0010375 305
7679  54
2518 15
73862397 17840


Satellite: ISS
Catalog Number: 25544
Epoch time:      10132
42555783   =   yrday
fracday
Element set:     902
Inclination:       51
6437  deg
RA of node:        54
1175  deg
Eccentricity:     
0010375     
Arg of perigee:   305
7679  deg
Mean anomaly:      54
2518  deg
Mean motion:   15
73862397  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1784
Checksum:              319


Coasting Arc #4 (Orbit 1799)
---------------------------------------

Vector Time (GMT): 2010/133/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1502710
79                 A    =         6727547
21  meter
 Y    =       -5645309
41  meter          E    =           
0007249
 Z    =       -3340581
01                 I    =           51
90229
 XDOT =       5977
578275                 Wp   =          333
67697
 YDOT =       1193
973596  meter/sec      RA   =           48
45718  deg
 ZDOT =      -4696
419921                 TA   =          245
43117
                                          MA   =          245
50674
                                          Ha   =            190
567  n
mi
                                          Hp   =            185
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4930153
51                 X    =        -1423243
93
 Y    =      -18521356
34  feet           Y    =        -5661669
02  meter
 Z    =      -10959911
45                 Z    =        -3347688
79
 XDOT =      19611
477280                 XDOT =        5986
597653
 YDOT =       3917
236206  feet/sec       YDOT =        1260
869259  meter/sec
 ZDOT =     -15408
201840                 ZDOT =       -4667
358172

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10983704
40                 X    =        -3347833
10
 Y    =      -15687048
50  feet           Y    =        -4781412
38  meter
 Z    =      -10988241
91                 Z    =        -3349216
13
 XDOT =      18694
287346                 XDOT =        5698
018783
 YDOT =      -2354
025468  feet/sec       YDOT =        -717
506963  meter/sec
 ZDOT =     -15292
457383                 ZDOT =       -4661
141010


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10133
44146056  
00016717  00000-0  10270-3 0  9038
2 25544  51
6447  48
9019 0010391 309
8849  50
1400 15
73914656 18001


Satellite: ISS
Catalog Number: 25544
Epoch time:      10133
44146056   =   yrday
fracday
Element set:     903
Inclination:       51
6447  deg
RA of node:        48
9019  deg
Eccentricity:     
0010391     
Arg of perigee:   309
8849  deg
Mean anomaly:      50
1400  deg
Mean motion:   15
73914656  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1800
Checksum:              293


Coasting Arc #5 (Orbit 1815)
---------------------------------------

Vector Time (GMT): 2010/134/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5300348
07                 A    =         6725160
35  meter
 Y    =        -567254
19  meter          E    =           
0009998
 Z    =        4104649
81                 I    =           51
87368
 XDOT =      -2293
380417                 Wp   =           15
75219
 YDOT =      -6276
318334  meter/sec      RA   =           43
28999  deg
 ZDOT =      -3817
244870                 TA   =          113
39138
                                          MA   =          113
28620
                                          Ha   =            190
759  n
mi
                                          Hp   =            185
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17389593
39                 X    =        -5313551
05
 Y    =       -1861070
17  feet           Y    =         -626600
10  meter
 Z    =       13466698
85                 Z    =         4078868
04
 XDOT =      -7524
213966                 XDOT =       -2204
483169
 YDOT =     -20591
595584  feet/sec       YDOT =       -6301
466811  meter/sec
 ZDOT =     -12523
769258                 ZDOT =       -3828
171097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16954040
94                 X    =        -5167591
68
 Y    =        4601849
80  feet           Y    =         1402643
82  meter
 Z    =       13364018
57                 Z    =         4073352
86
 XDOT =     -14076
020054                 XDOT =       -4290
370912
 YDOT =     -15251
306372  feet/sec       YDOT =       -4648
598182  meter/sec
 ZDOT =     -12567
297887                 ZDOT =       -3830
512396


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10134
45734708  
00016717  00000-0  10270-3 0  9048
2 25544  51
6451  43
6866 0010420 313
4656  46
5640 15
73933597 18165


Satellite: ISS
Catalog Number: 25544
Epoch time:      10134
45734708   =   yrday
fracday
Element set:     904
Inclination:       51
6451  deg
RA of node:        43
6866  deg
Eccentricity:     
0010420     
Arg of perigee:   313
4656  deg
Mean anomaly:      46
5640  deg
Mean motion:   15
73933597  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1816
Checksum:              307


Coasting Arc #6 (Orbit 1831)
---------------------------------------

Vector Time (GMT): 2010/135/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2479544
90                 A    =         6727431
86  meter
 Y    =        5283755
20  meter          E    =           
0009543
 Z    =        3332565
20                 I    =           51
85905
 XDOT =      -6101
198249                 Wp   =           35
17396
 YDOT =       -103
120283  meter/sec      RA   =           38
22186  deg
 ZDOT =       4704
010885                 TA   =            3
90906
                                          MA   =            3
90161
                                          Ha   =            190
871  n
mi
                                          Hp   =            185
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8134989
82                 X    =         2404087
43
 Y    =       17335154
84  feet           Y    =         5311060
61  meter
 Z    =       10933612
85                 Z    =         3344428
43
 XDOT =     -20017
054623                 XDOT =       -6122
443310
 YDOT =       -338
321139  feet/sec       YDOT =        -171
466906  meter/sec
 ZDOT =      15433
106578                 ZDOT =        4674
319125

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14033878
17                 X    =         4277526
07
 Y    =       12988473
26  feet           Y    =         3958886
65  meter
 Z    =       10980863
75                 Z    =         3346967
27
 XDOT =     -17791
079996                 XDOT =       -5422
721183
 YDOT =       6278
165287  feet/sec       YDOT =        1913
584779  meter/sec
 ZDOT =      15314
851244                 ZDOT =        4667
966659


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10135
47321728  
00016717  00000-0  10270-3 0  9056
2 25544  51
6452  38
4706 0010416 317
3796  42
6558 15
73953740 18329


Satellite: ISS
Catalog Number: 25544
Epoch time:      10135
47321728   =   yrday
fracday
Element set:     905
Inclination:       51
6452  deg
RA of node:        38
4706  deg
Eccentricity:     
0010416     
Arg of perigee:   317
3796  deg
Mean anomaly:      42
6558  deg
Mean motion:   15
73953740  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1832
Checksum:              309


Coasting Arc #7 (Orbit 1846)
---------------------------------------

Vector Time (GMT): 2010/136/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5310442
55                 A    =         6725002
51  meter
 Y    =        -393767
38  meter          E    =           
0005690
 Z    =       -4103741
26                 I    =           51
82653
 XDOT =       3373
593798                 Wp   =            4
63125
 YDOT =       5775
502450  meter/sec      RA   =           33
05049  deg
 ZDOT =       3817
336586                 TA   =          304
43008
                                          MA   =          304
48385
                                          Ha   =            191
141  n
mi
                                          Hp   =            184
978

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17422711
79                 X    =         5334386
52
 Y    =       -1291887
74  feet           Y    =         -334248
40  meter
 Z    =      -13463718
06                 Z    =        -4077884
71
 XDOT =      11068
221123                 XDOT =        3290
216196
 YDOT =      18948
498852  feet/sec       YDOT =        5812
761261  meter/sec
 ZDOT =      12524
070163                 ZDOT =        3833
523991

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15572180
20                 X    =         4746400
52
 Y    =       -8092563
75  feet           Y    =        -2466613
43  meter
 Z    =      -13360732
76                 Z    =        -4072351
34
 XDOT =      16988
265612                 XDOT =        5178
023359
 YDOT =      11938
576102  feet/sec       YDOT =        3638
877996  meter/sec
 ZDOT =      12588
538715                 ZDOT =        3836
986600


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10136
42558063  
00016717  00000-0  10270-3 0  9067
2 25544  51
6454  33
5806 0010479 320
9705  39
0701 15
73983219 18477


Satellite: ISS
Catalog Number: 25544
Epoch time:      10136
42558063   =   yrday
fracday
Element set:     906
Inclination:       51
6454  deg
RA of node:        33
5806  deg
Eccentricity:     
0010479     
Arg of perigee:   320
9705  deg
Mean anomaly:      39
0701  deg
Mean motion:   15
73983219  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1847
Checksum:              308


Coasting Arc #8 (Orbit 1862)
---------------------------------------

Vector Time (GMT): 2010/137/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3366707
16                 A    =         6727200
72  meter
 Y    =       -4771027
41  meter          E    =           
0008640
 Z    =       -3348220
65                 I    =           51
80913
 XDOT =       6029
950238                 Wp   =          351
72808
 YDOT =       -964
566643  meter/sec      RA   =           27
97876  deg
 ZDOT =      -4678
927144                 TA   =          227
53564
                                          MA   =          227
60871
                                          Ha   =            191
175  n
mi
                                          Hp   =            184
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11045627
16                 X    =        -3296841
28
 Y    =      -15652977
07  feet           Y    =        -4808284
83  meter
 Z    =      -10984975
87                 Z    =        -3364407
19
 XDOT =      19783
301307                 XDOT =        6063
017576
 YDOT =      -3164
588724  feet/sec       YDOT =        -896
950611  meter/sec
 ZDOT =     -15350
810839                 ZDOT =       -4649
553246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16436219
42                 X    =        -5009759
68
 Y    =       -9769944
44  feet           Y    =        -2977879
07  meter
 Z    =      -11049440
81                 Z    =        -3367869
56
 XDOT =      16112
745625                 XDOT =        4911
164867
 YDOT =      -9841
621276  feet/sec       YDOT =       -2999
726165  meter/sec
 ZDOT =     -15233
809896                 ZDOT =       -4643
265256


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10137
44141910  
00016717  00000-0  10270-3 0  9070
2 25544  51
6460  28
3644 0010520 325
1542  34
8932 15
74017846 18631


Satellite: ISS
Catalog Number: 25544
Epoch time:      10137
44141910   =   yrday
fracday
Element set:     907
Inclination:       51
6460  deg
RA of node:        28
3644  deg
Eccentricity:     
0010520     
Arg of perigee:   325
1542  deg
Mean anomaly:      34
8932  deg
Mean motion:   15
74017846  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1863
Checksum:              285


Coasting Arc #9 (Orbit 1878)
---------------------------------------

Vector Time (GMT): 2010/138/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5202506
71                 A    =         6725039
25  meter
 Y    =        1287105
68  meter          E    =           
0012396
 Z    =        4066245
67                 I    =           51
77383
 XDOT =      -4286
936894                 Wp   =           23
62646
 YDOT =      -5097
281215  meter/sec      RA   =           22
80321  deg
 ZDOT =      -3856
231595                 TA   =          106
07177
                                          MA   =          105
93523
                                          Ha   =            191
369  n
mi
                                          Hp   =            184
477

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17068591
56                 X    =        -5236265
83
 Y    =        4222787
66  feet           Y    =         1228738
88  meter
 Z    =       13340701
03                 Z    =         4040889
98
 XDOT =     -14064
753589                 XDOT =       -4210
886635
 YDOT =     -16723
363567  feet/sec       YDOT =       -5144
794586  meter/sec
 ZDOT =     -12651
678461                 ZDOT =       -3876
873515

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13715264
54                 X    =        -4180412
63
 Y    =       11124068
41  feet           Y    =         3390616
05  meter
 Z    =       13239700
83                 Z    =         4035460
81
 XDOT =     -18969
230662                 XDOT =       -5781
821506
 YDOT =      -8172
465098  feet/sec       YDOT =       -2490
967362  meter/sec
 ZDOT =     -12733
890042                 ZDOT =       -3881
289685


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10138
45724190  
00016717  00000-0  10270-3 0  9080
2 25544  51
6455  23
1481 0010509 328
8299  31
2240 15
74022901 18791


Satellite: ISS
Catalog Number: 25544
Epoch time:      10138
45724190   =   yrday
fracday
Element set:     908
Inclination:       51
6455  deg
RA of node:        23
1481  deg
Eccentricity:     
0010509     
Arg of perigee:   328
8299  deg
Mean anomaly:      31
2240  deg
Mean motion:   15
74022901  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1879
Checksum:              295


Coasting Arc #10 (Orbit 1894)
---------------------------------------

Vector Time (GMT): 2010/139/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4091155
76                 A    =         6726973
29  meter
 Y    =        4112906
42  meter          E    =           
0011983
 Z    =        3389726
34                 I    =           51
75298
 XDOT =      -5828
991137                 Wp   =           39
01951
 YDOT =       1975
405256  meter/sec      RA   =           17
72673  deg
 ZDOT =       4638
628895                 TA   =             
95121
                                          MA   =             
94893
                                          Ha   =            191
431  n
mi
                                          Hp   =            184
112

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13422427
02                 X    =         4028393
75
 Y    =       13493787
45  feet           Y    =         4158304
88  meter
 Z    =       11121149
41                 Z    =         3409449
17
 XDOT =     -19123
986669                 XDOT =       -5873
180877
 YDOT =       6480
988372  feet/sec       YDOT =        1909
974438  meter/sec
 ZDOT =      15218
598737                 ZDOT =        4610
204513

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17941413
64                 X    =         5468542
88
 Y    =        6212578
84  feet           Y    =         1893594
03  meter
 Z    =       11199703
22                 Z    =         3413669
54
 XDOT =     -13926
263803                 XDOT =       -4244
725207
 YDOT =      12988
527276  feet/sec       YDOT =        3958
903114  meter/sec
 ZDOT =      15105
372063                 ZDOT =        4604
117405


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10139
47304825  
00016717  00000-0  10270-3 0  9093
2 25544  51
6460  17
9309 0010579 332
8056  27
2552 15
74044836 18950


Satellite: ISS
Catalog Number: 25544
Epoch time:      10139
47304825   =   yrday
fracday
Element set:     909
Inclination:       51
6460  deg
RA of node:        17
9309  deg
Eccentricity:     
0010579     
Arg of perigee:   332
8056  deg
Mean anomaly:      27
2552  deg
Mean motion:   15
74044836  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1895
Checksum:              317


Coasting Arc #11 (Orbit 1909)
---------------------------------------

Vector Time (GMT): 2010/140/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4934049
83                 A    =         6724984
74  meter
 Y    =       -2156551
82  meter          E    =           
0007889
 Z    =       -4025213
96                 I    =           51
71787
 XDOT =       5059
324092                 Wp   =           17
65722
 YDOT =       4289
635662  meter/sec      RA   =           12
54647  deg
 ZDOT =       3912
791818                 TA   =          292
63637
                                          MA   =          292
71979
                                          Ha   =            191
673  n
mi
                                          Hp   =            183
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16187827
53                 X    =         4977351
85
 Y    =       -7075301
24  feet           Y    =        -2101133
89  meter
 Z    =      -13206082
55                 Z    =        -4001139
33
 XDOT =      16598
832323                 XDOT =        4991
972944
 YDOT =      14073
607814  feet/sec       YDOT =        4345
835136  meter/sec
 ZDOT =      12837
243496                 ZDOT =        3937
206787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11237342
89                 X    =         3425142
11
 Y    =      -13724120
95  feet           Y    =        -4183112
07  meter
 Z    =      -13110182
80                 Z    =        -3995983
72
 XDOT =      20126
328544                 XDOT =        6134
504940
 YDOT =       4153
172542  feet/sec       YDOT =        1265
886991  meter/sec
 ZDOT =      12934
487079                 ZDOT =        3942
431662


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10140
42535149  
00016717  00000-0  10270-3 0  9107
2 25544  51
6466  13
0404 0010652 336
0539  24
0128 15
74083254 19102


Satellite: ISS
Catalog Number: 25544
Epoch time:      10140
42535149   =   yrday
fracday
Element set:     910
Inclination:       51
6466  deg
RA of node:        13
0404  deg
Eccentricity:     
0010652     
Arg of perigee:   336
0539  deg
Mean anomaly:      24
0128  deg
Mean motion:   15
74083254  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1910
Checksum:              263


Coasting Arc #12 (Orbit 1925)
---------------------------------------

Vector Time (GMT): 2010/141/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4690647
74                 A    =         6726609
55  meter
 Y    =       -3370367
70  meter          E    =           
0010495
 Z    =       -3458946
14                 I    =           51
69453
 XDOT =       5464
339347                 Wp   =            6
73731
 YDOT =      -2916
348009  meter/sec      RA   =            7
46661  deg
 ZDOT =      -4559
650386                 TA   =          214
16134
                                          MA   =          214
22892
                                          Ha   =            191
704  n
mi
                                          Hp   =            183
535

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15389264
25                 X    =        -4635808
07
 Y    =      -11057636
80  feet           Y    =        -3422514
47  meter
 Z    =      -11348248
49                 Z    =        -3481600
39
 XDOT =      17927
622529                 XDOT =        5518
694386
 YDOT =      -9568
070896  feet/sec       YDOT =       -2854
938309  meter/sec
 ZDOT =     -14959
482894                 ZDOT =       -4532
972687

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18727325
29                 X    =        -5708088
75
 Y    =       -2516352
81  feet           Y    =         -766984
34  meter
 Z    =      -11438478
29                 Z    =        -3486448
18
 XDOT =      11182
340664                 XDOT =        3408
377434
 YDOT =     -15573
493625  feet/sec       YDOT =       -4746
800857  meter/sec
 ZDOT =     -14853
215936                 ZDOT =       -4527
260217


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10141
44112660  
00016717  00000-0  10270-3 0  9110
2 25544  51
6471   7
8238 0010715 339
3468  20
7261 15
74102291 19262


Satellite: ISS
Catalog Number: 25544
Epoch time:      10141
44112660   =   yrday
fracday
Element set:     911
Inclination:       51
6471  deg
RA of node:         7
8238  deg
Eccentricity:     
0010715     
Arg of perigee:   339
3468  deg
Mean anomaly:      20
7261  deg
Mean motion:   15
74102291  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1926
Checksum:              276


Coasting Arc #13 (Orbit 1941)
---------------------------------------

Vector Time (GMT): 2010/142/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4597026
98                 A    =         6725127
93  meter
 Y    =        2933925
57  meter          E    =           
0014636
 Z    =        3938010
08                 I    =           51
65923
 XDOT =      -5621
546329                 Wp   =           32
44441
 YDOT =      -3398
863530  meter/sec      RA   =            2
28152  deg
 ZDOT =      -4011
056487                 TA   =           99
27589
                                          MA   =           99
11033
                                          Ha   =            191
877  n
mi
                                          Hp   =            183
332

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15082109
51                 X    =        -4648623
29
 Y    =        9625740
07  feet           Y    =         2882230
17  meter
 Z    =       12919980
58                 Z    =         3915552
38
 XDOT =     -18443
393467                 XDOT =       -5563
636672
 YDOT =     -11151
127067  feet/sec       YDOT =       -3461
402994  meter/sec
 ZDOT =     -13159
634145                 ZDOT =       -4038
225707

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8549155
34                 X    =        -2605782
55
 Y    =       15790514
61  feet           Y    =         4812948
85  meter
 Z    =       12830525
66                 Z    =         3910744
22
 XDOT =     -20319
861266                 XDOT =       -6193
493714
 YDOT =       -169
661351  feet/sec       YDOT =         -51
712780  meter/sec
 ZDOT =     -13267
842884                 ZDOT =       -4044
038511


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10142
45688616  
00016717  00000-0  10270-3 0  9122
2 25544  51
6469   2
6070 0010792 343
6632  16
4182 15
74142691 19422


Satellite: ISS
Catalog Number: 25544
Epoch time:      10142
45688616   =   yrday
fracday
Element set:     912
Inclination:       51
6469  deg
RA of node:         2
6070  deg
Eccentricity:     
0010792     
Arg of perigee:   343
6632  deg
Mean anomaly:      16
4182  deg
Mean motion:   15
74142691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1942
Checksum:              298


Coasting Arc #14 (Orbit 1957)
---------------------------------------

Vector Time (GMT): 2010/143/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5097631
34                 A    =         6726216
19  meter
 Y    =        2560865
84  meter          E    =           
0013801
 Z    =        3545895
77                 I    =           51
63322
 XDOT =      -5011
336014                 Wp   =           44
20094
 YDOT =       3787
159665  meter/sec      RA   =          357
19689  deg
 ZDOT =       4468
601800                 TA   =          358
12137
                                          MA   =          358
12655
                                          Ha   =            191
920  n
mi
                                          Hp   =            183
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16724512
27                 X    =         5051390
86
 Y    =        8401790
81  feet           Y    =         2617611
82  meter
 Z    =       11633516
31                 Z    =         3570548
23
 XDOT =     -16441
391122                 XDOT =       -5075
020201
 YDOT =      12425
064517  feet/sec       YDOT =        3730
763559  meter/sec
 ZDOT =      14660
767061                 ZDOT =        4444
101961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18622697
73                 X    =         5676198
27
 Y    =       -1095680
99  feet           Y    =         -333963
57  meter
 Z    =       11731696
96                 Z    =         3575821
23
 XDOT =      -8135
124422                 XDOT =       -2479
585924
 YDOT =      17685
824380  feet/sec       YDOT =        5390
639271  meter/sec
 ZDOT =      14563
178985                 ZDOT =        4438
856955


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10143
47263040  
00016717  00000-0  10270-3 0  9136
2 25544  51
6472 357
3897 0010849 347
5434  12
5460 15
74136118 19589


Satellite: ISS
Catalog Number: 25544
Epoch time:      10143
47263040   =   yrday
fracday
Element set:     913
Inclination:       51
6472  deg
RA of node:       357
3897  deg
Eccentricity:     
0010849     
Arg of perigee:   347
5434  deg
Mean anomaly:      12
5460  deg
Mean motion:   15
74136118  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1958
Checksum:              309


Coasting Arc #15 (Orbit 1972)
---------------------------------------

Vector Time (GMT): 2010/144/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4115066
14                 A    =         6725285
16  meter
 Y    =       -3662454
80  meter          E    =           
0010016
 Z    =       -3854012
98                 I    =           51
59986
 XDOT =       6027
434983                 Wp   =           24
57430
 YDOT =       2450
778858  meter/sec      RA   =          352
00704  deg
 ZDOT =       4119
501722                 TA   =          288
41615
                                          MA   =          288
52502
                                          Ha   =            192
118  n
mi
                                          Hp   =            182
866

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13500873
16                 X    =         4174436
94
 Y    =      -12015927
83  feet           Y    =        -3616105
40  meter
 Z    =      -12644399
54                 Z    =        -3833877
73
 XDOT =      19775
049157                 XDOT =        5979
569821
 YDOT =       8040
613051  feet/sec       YDOT =        2517
913257  meter/sec
 ZDOT =      13515
425597                 ZDOT =        4148
667438

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5410532
71                 X    =         1649130
37
 Y    =      -17303296
37  feet           Y    =        -5274044
73  meter
 Z    =      -12564195
47                 Z    =        -3829566
78
 XDOT =      19754
590721                 XDOT =        6021
199252
 YDOT =      -3690
481079  feet/sec       YDOT =       -1124
858633  meter/sec
 ZDOT =      13631
575892                 ZDOT =        4154
904332


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10144
42487455  
00016717  00000-0  10270-3 0  9141
2 25544  51
6470 352
4990 0010923 349
9536  10
1407 15
74176502 19732


Satellite: ISS
Catalog Number: 25544
Epoch time:      10144
42487455   =   yrday
fracday
Element set:     914
Inclination:       51
6470  deg
RA of node:       352
4990  deg
Eccentricity:     
0010923     
Arg of perigee:   349
9536  deg
Mean anomaly:      10
1407  deg
Mean motion:   15
74176502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1973
Checksum:              307

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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